DE3275665D1 - Aircraft flight control system - Google Patents

Aircraft flight control system

Info

Publication number
DE3275665D1
DE3275665D1 DE8282107195T DE3275665T DE3275665D1 DE 3275665 D1 DE3275665 D1 DE 3275665D1 DE 8282107195 T DE8282107195 T DE 8282107195T DE 3275665 T DE3275665 T DE 3275665T DE 3275665 D1 DE3275665 D1 DE 3275665D1
Authority
DE
Germany
Prior art keywords
control system
flight control
aircraft flight
aircraft
flight
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired
Application number
DE8282107195T
Other languages
German (de)
Inventor
Antonius Adrianus Lambregts
Rolf Hansen
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Boeing Co
Original Assignee
Boeing Co
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Boeing Co filed Critical Boeing Co
Application granted granted Critical
Publication of DE3275665D1 publication Critical patent/DE3275665D1/en
Expired legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/04—Control of altitude or depth
    • G05D1/06—Rate of change of altitude or depth
    • G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
    • G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
    • G05D1/0676—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for landing
DE8282107195T 1981-09-14 1982-08-09 Aircraft flight control system Expired DE3275665D1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/301,911 US4419732A (en) 1981-09-14 1981-09-14 Method and apparatus for an aircraft inner loop elevator control system

Publications (1)

Publication Number Publication Date
DE3275665D1 true DE3275665D1 (en) 1987-04-16

Family

ID=23165419

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8282107195T Expired DE3275665D1 (en) 1981-09-14 1982-08-09 Aircraft flight control system

Country Status (3)

Country Link
US (1) US4419732A (en)
EP (1) EP0074493B1 (en)
DE (1) DE3275665D1 (en)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5036469A (en) * 1989-03-02 1991-07-30 The Boeing Company Pitch attitude command flight control system for landing flare
US5377937A (en) * 1991-09-03 1995-01-03 The Boeing Company Aircraft flare control system utilizing an envelope limiter
US5901927A (en) * 1996-07-18 1999-05-11 Honeywell Inc. Ground strike protection function for aircraft autopilot
WO2002040477A2 (en) * 2000-11-03 2002-05-23 President And Fellows Of Harvard College Saframycins, analogues and uses thereof
US6676088B1 (en) * 2002-10-07 2004-01-13 Safe Flight Instrument Corporation Flare control system
US7183054B2 (en) * 2003-06-03 2007-02-27 President And Fellows Of Harvard College Assay for identifying biological targets of polynucleotide-binding compounds
CA2568848C (en) * 2004-07-16 2013-06-25 Airbus France Method and device for improving maneuverability of an aircraft during approach phases before landing followed by flare-out
US8019492B2 (en) * 2007-10-26 2011-09-13 The Boeing Company Operator fine tracking assist using sensor derived inputs
US8275496B2 (en) * 2007-11-21 2012-09-25 The Boeing Company Longitudinal and vertical gust feed forward compensation using lateral control surfaces
US8781653B2 (en) * 2012-01-11 2014-07-15 The Boeing Company Quiet landing attitude modifier for airplane
US10816998B2 (en) 2017-09-18 2020-10-27 The Boeing Company Airplane takeoff trims utilizing both stabilizers and elevators

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3447765A (en) * 1965-05-27 1969-06-03 Bendix Corp Automatic control system for landing an aircraft
US3291421A (en) * 1965-09-20 1966-12-13 Lear Siegler Inc Pitch controller for automatic landing
US3333795A (en) * 1966-01-10 1967-08-01 Collins Radio Co Flare computer
US3523663A (en) * 1968-03-28 1970-08-11 Bendix Corp Terminal flare controller
US3601339A (en) * 1968-06-03 1971-08-24 Elliott Brothers London Ltd Aircraft-landing systems
US3604908A (en) * 1969-05-19 1971-09-14 Sperry Rand Corp Landing control system for aircraft
US3578269A (en) * 1969-06-11 1971-05-11 Lear Siegler Inc Automatic flare and altitude hold system
US3626163A (en) * 1970-01-28 1971-12-07 Us Army Automatic landing system
US3652835A (en) * 1970-05-14 1972-03-28 Sperry Rand Corp Aircraft glide slope coupler system
US3847328A (en) * 1972-01-31 1974-11-12 Boeing Co Automatic go-around control system for aircraft
US3801049A (en) * 1972-01-31 1974-04-02 Boeing Co Automatic approach landing and go-around pitch axis control system for aircraft
US4006871A (en) * 1972-06-19 1977-02-08 The Boeing Company Automatic pitch axis control system for aircraft
US4164340A (en) * 1973-03-19 1979-08-14 The Boeing Company Method and apparatus for determining when a glide slope signal exceeds a predetermined level
US3892373A (en) * 1973-12-07 1975-07-01 Bendix Corp Integrated glide path/flare automatic flight control system
US3887148A (en) * 1973-12-19 1975-06-03 Sperry Rand Corp Aircraft glide slope coupler and landing system
US3918662A (en) * 1974-01-21 1975-11-11 Boeing Co Localizer lateral guidance control system
US3976267A (en) * 1974-11-14 1976-08-24 The Boeing Company Vertical glide slope control system including complementary filter
US4032093A (en) * 1975-06-27 1977-06-28 The Boeing Company Adaptive energy management for vertical speed control of an aircraft
US4104612A (en) * 1977-02-03 1978-08-01 Mcdonnell Douglas Corporation Head-up display command bar generator
US4141522A (en) * 1977-05-16 1979-02-27 Boeing Commercial Airplane Company Independent glide slope gain programming system
US4357661A (en) * 1980-02-22 1982-11-02 The Boeing Company Aircraft landing control system
US4326253A (en) * 1980-03-31 1982-04-20 The Boeing Company Lift control system for aircraft vertical path guidance
US4354237A (en) * 1980-06-24 1982-10-12 The Boeing Company Method and apparatus for producing an aircraft flare path control signal

Also Published As

Publication number Publication date
US4419732A (en) 1983-12-06
EP0074493B1 (en) 1987-03-11
EP0074493A1 (en) 1983-03-23

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee